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C19200 Copper vs. C85400 Brass

Both C19200 copper and C85400 brass are copper alloys. They have 68% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.

For each property being compared, the top bar is C19200 copper and the bottom bar is C85400 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
100
Elongation at Break, % 2.0 to 35
23
Poisson's Ratio 0.34
0.32
Shear Modulus, GPa 44
40
Tensile Strength: Ultimate (UTS), MPa 280 to 530
220
Tensile Strength: Yield (Proof), MPa 98 to 510
85

Thermal Properties

Latent Heat of Fusion, J/g 210
180
Maximum Temperature: Mechanical, °C 200
130
Melting Completion (Liquidus), °C 1080
940
Melting Onset (Solidus), °C 1080
940
Specific Heat Capacity, J/kg-K 390
380
Thermal Conductivity, W/m-K 240
89
Thermal Expansion, µm/m-K 17
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 58 to 74
20
Electrical Conductivity: Equal Weight (Specific), % IACS 58 to 75
22

Otherwise Unclassified Properties

Base Metal Price, % relative 30
25
Density, g/cm3 8.9
8.3
Embodied Carbon, kg CO2/kg material 2.6
2.8
Embodied Energy, MJ/kg 41
46
Embodied Water, L/kg 310
330

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 98
40
Resilience: Unit (Modulus of Resilience), kJ/m3 42 to 1120
35
Stiffness to Weight: Axial, points 7.2
7.0
Stiffness to Weight: Bending, points 18
19
Strength to Weight: Axial, points 8.8 to 17
7.5
Strength to Weight: Bending, points 11 to 16
9.9
Thermal Diffusivity, mm2/s 69
28
Thermal Shock Resistance, points 10 to 19
7.6

Alloy Composition

Aluminum (Al), % 0
0 to 0.35
Copper (Cu), % 98.5 to 99.19
65 to 70
Iron (Fe), % 0.8 to 1.2
0 to 0.7
Lead (Pb), % 0 to 0.030
1.5 to 3.8
Nickel (Ni), % 0
0 to 1.0
Phosphorus (P), % 0.010 to 0.040
0
Silicon (Si), % 0
0 to 0.050
Tin (Sn), % 0
0.5 to 1.5
Zinc (Zn), % 0 to 0.2
24 to 32
Residuals, % 0
0 to 1.1